N13566

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,544 hrs · 26,003 cycles

THE CREW REPORTED THE AFT THREE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT DC/AC INVERTER. OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,283 hrs · 25,783 cycles

DURING MAINTENANCE INSPECTION THE NR 2 EMERGENCY LIGHT FLOOR STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,184 hrs · 25,701 cycles

DURING ROUTINE MAINTENANCE, THE LAST EMERGENCY AILSE PATH LIGHTING STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LAST EMERGENCY AISLE PATH LIGHT STRIP. OPS CHECKS WERE GOOD.

Part: CONTROL MODULE — SHORTED (CABIN LIGHTS) · airframe 33,054 hrs · 25,590 cycles

CREW REPORTED A BURNING ODOR IN FRONT CABIN NEAR MAIN CABIN DOOR. MAINTENANCE R & R CABIN LIGHT CONTROL MODULE WITH OPS CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: ACM — FROZEN (RIGHT) · airframe 31,767 hrs · 24,532 cycles

THE CREW REPORTED CABIN SMOKE DURING FLIGHT. THE ACFT DIVERTED TO LT WHERE OT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE NR 2 PACK TO CURRENTLY BE ON DEFERRAL AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D, WHERE MAINTENANCE R & R THE NR 2 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,974 hrs · 23,093 cycles

DURING MAINTENANCE INSPECTION, THE MAIN CABIN DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R THE MAIN CABIN DOOR EMERGENCY LIGHT BULB WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 77) · airframe 28,493 hrs · 21,939 cycles

DURING C-CHECK, FUSELAGE CRACKED AROUND THREE RIVETS AT FRAME 77 S3-5L. MAINTENANCE REPAIRED FUSELAGE SKIN IAW EC5330-02859. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 28,493 hrs · 21,939 cycles

DURING C-CHECK, CARGO LOWER BEAM CORRODED BETWEEN FRAMES 65-68. MAINTENANCE R & R CARGO LOWER BEAM IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 27,100 hrs · 20,865 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,874 hrs · 20,695 cycles

THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MX INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,674 hrs · 20,542 cycles

DURING SCHEDULED MX INSPECTION THE OVERHEAD GALLEY EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE OVERHEAD GALLEY EMERGENCY LIGHT BULB WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,674 hrs · 20,542 cycles

DURING SCHEDULED MX INSPECTION BOTH AFT OVERWING EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,456 hrs · 20,369 cycles

DURING SCHEDULED MX INSPECTION, THE FLOOR PROXIMITY EMERGENCY LIGHTS NEAR THE LAVATORY WERE FOUND INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,456 hrs · 20,369 cycles

DURING SCHEDULED MX INSPECTION EXTERNAL OVERWING EMERGENCY LIGHTS FOUND INOPERATIVE. MX R & R BATTERY CHARGER ASSY, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (ZONE 200) · airframe 25,413 hrs · 19,565 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED A DENT IN THE CENTER FUSELAGE I SKIN 8" AFT OF THE PAX DOOR. MX INSPECTED THE ACFT, CUT OUT THE DAMAGED SECTION, AND APPLIED A DOUBLER REPAIR. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,411 hrs · 18,728 cycles

DURING MX INSPECTION, EMERGENCY LIGHT AT ROW 18A AND 19A WAS FOUND INOPERATIVE. MX RESET SYS AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (NR 4 BATTERY) · airframe 24,304 hrs · 18,642 cycles

DURING ROUTINE MX, THE LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE FUSE ON THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,919 hrs · 18,340 cycles

DURING SCHEDULED MX INSPECTION, THE LT & RT AFT EXTERNAL OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. R & R BATTERY CHARGER IAW AMM 33-50-04 WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — FAULTY (FUEL CELL) · airframe 22,892 hrs · 17,589 cycles

THE CREW REPORTED FUEL LEAKING FROM WING AFTER TAKE OFF. THE ACFT RETURNED TO AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE FLAP VALVE ON THE NR2 RT FUEL TANK. PERFORMED LEAK CHECK. NO LEAKS FOUND.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 22,303 hrs · 17,075 cycles

TYS FOR BNA. THE LAV SMOKE TEST FAIL. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR IAW EMB 145 MM 26-14-01. OPS CHECK GOOD AND A/C RELEASED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,007 hrs · 16,827 cycles

DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHT STRIP AT EXIT ROW WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 21,337 hrs · 16,282 cycles

CLE FLT 2362 THE CREW REPORTED LAV SMOKE INOPERATIVE MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 21,328 hrs · 16,275 cycles

FLIGHT 2416 - FLIGHT CREW REPORTED LAV SMOKE WARNING ON EICAS. MX REMOVED AND REPLACED SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 16,985 hrs · 13,244 cycles

MCI - DURING MAINTENANCE INSPECTION THE AFT OVERWING EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — BURNED (COCKPIT) · airframe 18,776 hrs · 14,301 cycles

FLIGHT 2087 - EWR - FLIGHT CREW REPORTED 115VAC OFF BUSS ACRID BURNING SMELL IN COCKPIT RADIATING FROM CENTER CONSOLE. EWR MX REMOVED AND REPLACED INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 18,650 hrs · 14,215 cycles

IAH - FLIGHT 2151, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT AN AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY, AND POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,650 hrs · 14,215 cycles

IAH - FLIGHT 2151, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT AN AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY, AND POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 18,563 hrs · 14,151 cycles

SHV - DURING C-CHECK, SERVICE DOOR CUTOUT AFT FRAME HAS CORROSION. REPAIRED FRAME IAW EC 5310-01373. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 18,563 hrs · 14,151 cycles

SHV - DURING C-CHECK, SERVICE DOOR CUTOUT FWD FRAME HAS CORROSION. REPAIRED FRAME IAW EC 5310-01373. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,563 hrs · 14,151 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 54-58. REPAIRED OMEGA BEAM IAW EC 5320-01540. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 17,909 hrs · 13,672 cycles

FLIGHT 3067 - SDF - FLIGHT CREW REPORTED AIR/GRND FAIL ON EICAS. RESET THE SYSTEM AND FALSE INDICATION WAS CLEARED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: O-RING — BLOWN (BLEED AIR SYS) · airframe 17,761 hrs · 13,567 cycles

IAH - FLIGHT 2617 THE CREW REPORTED A BLEED ONE LEAK IN CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED O-RINGS IN THE LEFT CARGO WALL AT LOCATION 19, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ROLLER — OUT OF ADJUST (MAIN DOOR) · airframe 16,696 hrs · 12,749 cycles

FLIGHT 2399 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR STUCK AND HARD TO OPEN. EWR MX PERFORMED MAIN DOOR ACTUATING HANDLE TEST AND ADJUSTMENT, PERFORMED MAIN DOORS ROLLERS ADJUSTMENT AND LUBRICATION. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 2 ENGINE) · airframe 16,500 hrs · 12,595 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.

Part: THRUST REVERSER — MALFUNCTIONED (NR 2 ENGINE) · airframe 16,300 hrs · 12,449 cycles

CLE FLIGHT 2333 - THE CREW REPORTED A ENGINE THRUST REVERSER DISAGREE ON TAKEOFF. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND VERIFIED THE NR 2 REVERSER WAS AT FAULT. THE SYSTEM WAS PLACED ON MEL. SUPPLEMENT TO FOLLOW:

Part: SEQUENCE VALVE — MALFUNCTIONED (NLG) · airframe 15,066 hrs · 11,529 cycles

FLIGHT 2825 EWR FLIGHT CREW REPORTED THAT DURING CLIMBING OUT OF EWR THEY HEARD A SOUND LIKE GEAR WAS STILL DOWN WITH GEAR LEVER UP AND GEAR INDICATION SHOWING UP POSITION. CREW RECYCLE GEAR TWICE AT AIR SPEED UNDER 200 KT. NOISE ONLY SLIGHTLY CHANGED WHEN GEAR WENT UP. FLIGHT CREW AIR RETURNED TO EWR UNEVENTFULLY. EWR MX R&R NLG SEQUENCE VALVE. R&R NLG RT DOOR AND THIRD UPPER LOCK BOX PROXIMITY SW. EWR MX PREFORMED LEAK AND OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SEQUENCE VALVE — MALFUNCTIONED (MLG) · airframe 15,066 hrs · 11,529 cycles

FLIGHT 2825 - FLIGHT CREW REPORTED THAT DURING CLIMBING OUT, THEY HEARD A SOUND LIKE GEAR WAS STILL DOWN WITH GEAR LEVER UP AND GEAR INDICATION SHOWING UP POSITION. CREW RECYCLED GEAR TWICE AT AIR SPEED UNDER 200KNT, NOISE ONLY SLIGHTLY CHANGED WHEN GEAR WENT UP. FLIGHT CREW AIR RETURNED TO DEPARTURE UNEVENTFULLY. MX REMOVED AND REPLACED NOSE LANDING GEAR SEQUENCE VALVE , REMOVED AND REPLACED NOSE LANDING GEAR RT DOOR, AND THIRD UPPER LOCK BOX PROXIMITY SW. MX PERFORMED LEAK AND OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K)

Part: UNKNOWN — MALFUNCTIONED (NLG)

FLIGHT CREW REPORTED THAT DURING CLIMBING OUT, THEY HEARD A SOUND LIKE GEAR WAS STILL DOWN WITH GEAR LEVER UP AND GEAR INDICATION SHOWING UP POSITION. CREW RECYCLE GEAR TWICE AT AIR SPEED UNDER 200 KT, NOISE ONLY SLIGHTLY CHANGED WHEN GEAR WENT UP. FLIGHT CREW AIR RETURNED TO DEPARTURE UNEVENTFULLY. MX REMOVED AND REPLACED NLG SEQUENCE VALVE , REMOVED AND REPLACED NOSE LANDING GEAR RT DOOR AND THIRD UPPER LOCK BOX PROXIMITY SW. MX PERFORMED LEAK AND OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K)

Part: SEQUENCE VALVE — MALFUNCTIONED (NLG)

FLIGHT CREW REPORTED THAT DURING CLIMBING OUT, THEY HEARD A SOUND LIKE GEAR WAS STILL DOWN WITH GEAR LEVER UP AND GEAR INDICATION SHOWING UP POSITION. CREW RECYCLE GEAR TWICE AT AIR SPEED UNDER 200 KT. NOISE ONLY SLIGHTLY CHANGED WHEN GEAR WENT UP. FLIGHT CREW AIR RETURNED TO DEPARTURE UNEVENTFULLY. MX REMOVED AND REPLACED NLG SEQUENCE VALVE, REMOVED AND REPLACED NLG RT DOOR, AND THIRD UPPER LOCK BOX PROXIMITY SWITCH. MX PERFORMED LEAK AND OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K)

Part: COFFEEMAKER — BURNED (GALLEY) · airframe 14,333 hrs

IAH - FLIGHT 2504, THE CREW REPORTED A BURNING SMELL IN FRONT OF CABIN. MAINTENANCE INSPECTED THE ACFT AND FOUND THE NR1 COFFEE BREWER TO BE BURNED UP. MAINTENANCE REMOVED AND REPLACED THE COFFEE BREWER. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: BEAM — CORRODED (CARGO DOOR) · airframe 13,619 hrs · 10,564 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER BEAM HAS VARIOUS AREAS OF CORROSION. MX REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SMOKE — DETECTED (COCKPIT) · airframe 8,790 hrs · 6,912 cycles

GSO FLIGHT 2311, THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT DIVERTED INTO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE WINDSHIELD HEAT WIRING/ PITOT HEAT RELAYS AND CURRENT SENSORS. OPERATED WINDSHIELD HEAT AND PITOT HEAT/AIR CONDITIONING PACKS AND FANS. RESECURED DUCT ON NR 1 PACK DUAL TEMP CONTROLLER. NO DEFECTS WERE FOUND AND THE AIRCRAFT WAS TEST FLOWN. TEST FIGHT WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 6,886 hrs · 5,434 cycles

CLE FLIGHT 2441 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO CLOSE. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR IAW 52-18-05. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 4,138 hrs · 3,354 cycles

DURING C-CHECK, THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 4,138 hrs · 3,354 cycles

DURING C-CHECK, THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 4,138 hrs · 3,354 cycles

DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (FUSELAGE) · airframe 4,138 hrs · 3,354 cycles

DURING C CHECK THE T REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — FAULTY

BDL---CO3368, CREW REPORTED EMERGENCY FLOOR EXIT LIGHTING PROXIMITY STRIP NEAR EXIT INOPERATIVE....CONTRACT MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT STRIP AND OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.